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Aerospace Engineering Department, Graduate School of Engineering, Nagoya University | 論文
- Energy Separation in High Subsonic Turbine Cascade
- Novel Flow Control Method for Vortex Shedding of Turbine Blade
- Control of Leakage Flow by Triple Squealer Configuration in Axial Flow Turbine
- Visualization of Pressure Field over Rotating Blades Using Pressure Sensitive Foil Technique
- Visualization of Pressure Field over Rotating Blades Using Pressure Sensitive Foil Technique
- Comparison between Hot and Cold Flow Conditions of Turbine Cascade